US7950364B2 - Prechamber for a gas engine - Google Patents
Prechamber for a gas engine Download PDFInfo
- Publication number
- US7950364B2 US7950364B2 US11/664,077 US66407705A US7950364B2 US 7950364 B2 US7950364 B2 US 7950364B2 US 66407705 A US66407705 A US 66407705A US 7950364 B2 US7950364 B2 US 7950364B2
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- US
- United States
- Prior art keywords
- prechamber
- graduated
- cavities
- set forth
- cross
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/10—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
- F02B19/1004—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder details of combustion chamber, e.g. mounting arrangements
- F02B19/1014—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder details of combustion chamber, e.g. mounting arrangements design parameters, e.g. volume, torch passage cross sectional area, length, orientation, or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/16—Chamber shapes or constructions not specific to sub-groups F02B19/02 - F02B19/10
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/10—Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/12—Engines characterised by precombustion chambers with positive ignition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a device for a prechamber unit of a gas engine, comprising a prechamber unit in the form of an elongated body arranged to be placed in an upper part of the engine's cylinder, and where the elongated body comprises a prechamber gas valve and an ignition means arranged side by side, and one or more channels for supply of fuel gas via the prechamber gas valve to a prechamber in a lower part of the elongated body and where said prechamber comprises an elongated cavity in the axial direction with nozzles placed at the end for supply of ignited fuel gas to the engine's cylinder with the help of the ignition means.
- the invention relates in the main to a prechamber for a lean-burn gas engine, even if the invention can, in principle, also be used in other gas engines.
- a lean-burn gas engine Otto engine
- the cylinder is filled with a homogenous, lean mixture of air and fuel gas.
- an ignition amplifier in the form of a prechamber is often used, where the charge is made richer in that the fuel gas is supplied through a separate prechamber gas valve, and where an ignition means in the form of, for example, a spark plug or pilot injection valve is located.
- an ignition means in the form of, for example, a spark plug or pilot injection valve is located.
- the prechamber is a substantial contributor to the formation of NOx during the combustion. Furthermore, the prechamber is subjected to high thermal loads and requires much cooling. Reduced size and subsequent reduced amount of energy released in the prechamber also leads to a gain in the form of lower thermal load and reduced Wear on the ignition means and prechamber gas valve.
- Prechambers of these types are mainly intended for use in engines with bores from around 200 mm and upward. This is due to physical limitations in relation to how small the prechamber in reality can be made, but must not be viewed as limiting for the invention.
- the technology is applicable both to stationary engines and for propulsion engines with variable revolutions per minute.
- the volume of the prechamber can constitute a very small part of the compression volume. In an advantageous embodiment, it is probable that this volume can be less than 1.2% of the compression volume. However, it must be pointed out that the volume can also be greater if this is required.
- the prechamber gas valve can be placed as close to the prechamber as possible to achieve a rapid valve response, minimal transport delay and good control of the formation of the mixture in the prechamber.
- the shape of the prechamber gas valve can also be modified to contribute further to the above mentioned advantages.
- the ignition means and the prechamber gas supply can be placed outside the central line of the prechamber to achieve a compact design, good mixture formation and good cooling and the nozzle part of the prechamber can be specially made to provide an optimal distribution of the released energy.
- Prechambers for such gas engines are, of course, previously known.
- a relatively large amount of a rich charge must be used, which thereby contributes to formation of much NOx during the combustion.
- Use of a relatively large amount of rich charge leads to much heat being formed in the prechamber. This in turn leads to material thickness and material quality, etc., for the prechamber having to be increased to adapt to the development of heat. The complexity and manufacturing costs will thereby also increase.
- a prechamber of a gas engine that is divided into two chambers, namely a first and a second chamber, is known.
- the second chamber has a supply of fuel and a spark plug.
- nozzles at the opening from the prechamber to the main combustion chamber itself are not known from this document.
- This object is achieved with a prechamber divided into several connected and, in cross-section, graduated cavities where an upper cavity is widest in the cross-sectional direction and a cavity at the bottom is narrowest in the cross-sectional direction
- the elongated cavity can be arranged centrally in the center line of the elongated body, and that the uppermost cavity that receives fuel gas frnm the prechamber gas valve and which comprises the ignition mechanism of the ignition means, runs over into a cavity, smaller in the cross-sectional direction, and which in turn runs over into an even smaller cavity in the cross-sectional direction.
- the bottom cavity preferably comprises said nozzles for supply of ignited fuel gas to the engine's cylinder.
- the uppermost cavity can be shaped as a cylindrical chamber with rounded corners in cross-section.
- the middle cavity can be in the form of a circular-cylindrical boring, where a shoulder is provided in the transition between the uppermost chamber and said boring.
- the bottom cavity can be shaped as a mainly circular-cylindrical boring, where a shoulder is provided in the transition between the boring of the middle cavity and the boring of the bottom cavity. Said shoulders can be arranged to generate turbulence during injection in the prechamber.
- the lower part of the elongated body encompassing the whole or parts of the prechamber, can be releasable attached.
- the prechamber can be manufactured integrated with the elongated body.
- prechamber gas valve and the ignition means are arranged side by side in their own separate boring in the elongated body, where each boring is placed, cross-sectionally, completely, or partially, on each side of the center line of the elongated body.
- a non-return valve can be arranged as a prechamber gas valve.
- the prechamber can be divided into more than three connected and cross-sectionally graduated or tapered cavities, where the uppermost cavity is widest in the cross-sectional direction and the bottom cavity is narrowest in the cross-sectional direction.
- the volume of the prechamber can also constitute less than, or correspond to, 1.2% of the compression volume.
- FIG. 1 shows an embodiment of the present invention.
- FIG. 2 shows an alternative embodiment of the present invention.
- the prechamber volume i.e. the volume of the nozzle part independent of the construction/division.
- the whole unit can be defined as a prechamber unit, which in the main is comprised of a prechamber retainer (upper part) and a prechamber nozzle (lower part).
- FIGS. 1 and 2 shows a partial cross-section of two prechamber units.
- the difference between the two units is in the shape of the prechamber. Otherwise they are formed similarly.
- the form of the prechamber can in practice be different from what is shown in the figures, i.e. it can have any form which lies between what is shown and indeed also outside what is shown.
- the prechamber unit 10 comprises an elongated body 12 and which, in an upper part, comprises two separate borings 14 , 16 arranged side by side. Each boring 14 , 16 are placed completely, or partially, aside the center line 18 of the elongated body 12 .
- the one boring 14 preferably comprises a prechamber gas valve 20 , for example in the form of a non-return valve such as a ball valve, and the other boring 16 comprises preferably an ignition means 22 , for example in the form of a spark plug, a pilot injection valve, or another similar ignition mechanism.
- the prechamber gas valve 20 can be any type suitable for use in a prechamber unit of a gas engine.
- Supply of fuel gas to the prechamber gas valve 20 is brought about in a known way and will therefore not be described in more detail as it is known to one skilled in the art.
- fuel gas is supplied via a channel 24 , or more channels, to a prechamber 26 in the lower part of the elongated body 12 . It is important that the prechamber gas valve is placed as close to the prechamber as possible, i.e. that the channel 24 is as short as possible, to achieve fast valve response, minimal transport delay and good control of the mixture formation in the prechamber.
- the prechamber 26 comprises a cavity 28 extending in the axial direction.
- the elongated cavity 28 is divided into several connected and, in cross-section, graduated or tapered cavities 28 a , 28 b , 28 c .
- the uppermost cavity 28 a is preferably widest in the cross-sectional direction and the bottom cavity 28 c is preferably narrowest in the cross-sectional direction.
- the middle cavity 28 b if provided, has consequently a cross-section that lies between the other two cavities.
- the bottom cavity 28 c comprises nozzles 30 for supply of ignited fuel gas to the engine's cylinder.
- the elongated cavity 28 is arranged centrally in the center line of the elongated body 12 .
- the uppermost cavity 28 a which receives fuel gas from the prechamber gas valve 20 , and which comprises the ignition mechanism of the ignition means 22 runs by definition over into a cavity 28 b which is narrower in the cross-sectional direction and which in turn runs into an even narrower cavity 28 c in the cross-sectional direction.
- a form for the prechamber is not previously known, and the relative amount of energy which is released in the prechamber is thereby as small as possible.
- FIG. 1 show that the uppermost cavity 28 a is preferably formed as a cylindrical chamber with rounded corners in cross section, but it can of course be formed in other ways than shown here.
- the preferred form for the middle cavity 28 b is as a circular-cylindrical boring where a shoulder 32 is provided in the transition between the uppermost chamber and said boring.
- the bottom cavity 28 c is also preferably shaped as a mainly circular-cylindrical boring, where a shoulder 34 is provided in the transition between the boring of the middle cavity 28 b and the boring of the bottom cavity 28 c .
- FIG. 2 shows an alternative embodiment of the same cavities as shown in FIG. 1 by definition, but in the longitudinal direction, the middle and the bottom boring differ from what is shown in FIG. 1 .
- FIG. 1 shows that the uppermost cavity 28 a is preferably formed as a cylindrical chamber with rounded corners in cross section, but it can of course be formed in other ways than shown here.
- the preferred form for the middle cavity 28 b is as a circular-
- the bottom boring with the nozzles is much longer in the longitudinal direction and the middle boring is much shorter in the longitudinal direction than shown in FIG. 1 .
- the different chambers and borings shall be depends on the type of motor which the prechamber unit is to be mounted on, and also the area of application of the engine.
- the embodiments shown in FIGS. 1 and 2 are only examples of shapes of the prechamber and the prechamber can therefore have other forms than what is shown here.
- the shoulder 32 in the transition between the upper chamber 28 a and the middle boring 28 b will contribute to formation of turbulence in the prechamber.
- the shoulder 34 in the transition between the middle boring 28 b and the bottom boring 28 c will also contribute to the mentioned formation of turbulence in the prechamber.
- the degrees of the shoulders 32 , 34 can vary depending on the required turbulence, type of engine, etc.
- prechamber with three connected cavities is shown in the figures. However, it shall be pointed out that the prechamber can alternatively be shaped with only two connected cavities, or alternatively more than three connected cavities.
- the prechamber is, as mentioned, a substantial contributor to formation of NOx during the combustion, and furthermore, the prechamber is exposed to high thermal loads and requires good cooling.
- a prechamber unit of a reduced size and with a reduced amount of energy released in the prechamber is provided. This also gives a gain in the form of a lower thermal load and reduced wear on the ignition means and the prechamber gas valve. Calculations and tests have shown that the lifetime of the components can at least be doubled.
- reduced thermal load can yield a gain in the manufacture of the prechamber unit, for example, in that the material thickness or quality of the material can be reduced.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Description
Claims (11)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NO20044078A NO322345B1 (en) | 2004-09-27 | 2004-09-27 | Device at a front chamber of a gas engine |
NO20044078 | 2004-09-27 | ||
PCT/NO2005/000357 WO2006043818A1 (en) | 2004-09-27 | 2005-09-27 | Prechamber for a gas engine |
Publications (2)
Publication Number | Publication Date |
---|---|
US20100132660A1 US20100132660A1 (en) | 2010-06-03 |
US7950364B2 true US7950364B2 (en) | 2011-05-31 |
Family
ID=35057649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/664,077 Active 2028-05-04 US7950364B2 (en) | 2004-09-27 | 2005-09-27 | Prechamber for a gas engine |
Country Status (7)
Country | Link |
---|---|
US (1) | US7950364B2 (en) |
EP (1) | EP2054593B1 (en) |
KR (1) | KR100954004B1 (en) |
DK (1) | DK2054593T3 (en) |
ES (1) | ES2501265T3 (en) |
NO (1) | NO322345B1 (en) |
WO (1) | WO2006043818A1 (en) |
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120103302A1 (en) * | 2010-11-01 | 2012-05-03 | William Attard | Turbulent jet ignition pre-chamber combustion system for spark ignition engines |
US20120325179A1 (en) * | 2011-06-22 | 2012-12-27 | Caterpillar Inc. | Pre-combustion chamber tip |
US20140190437A1 (en) * | 2013-01-08 | 2014-07-10 | Woodward, Inc. | Quiescent Chamber Hot Gas Igniter |
US20140196686A1 (en) * | 2013-01-11 | 2014-07-17 | Caterpillar Inc. | Gaseous common rail fuel system and high compression ratio engine using same |
US8839762B1 (en) | 2013-06-10 | 2014-09-23 | Woodward, Inc. | Multi-chamber igniter |
US9172217B2 (en) | 2010-11-23 | 2015-10-27 | Woodward, Inc. | Pre-chamber spark plug with tubular electrode and method of manufacturing same |
US9353674B2 (en) | 2010-11-01 | 2016-05-31 | Mahle Powertrain, Llc | Turbulent jet ignition pre-chamber combustion system for spark ignition engines |
US20160252045A1 (en) * | 2015-02-27 | 2016-09-01 | Ge Jenbacher Gmbh & Co Og | Cylinder head |
US9476347B2 (en) | 2010-11-23 | 2016-10-25 | Woodward, Inc. | Controlled spark ignited flame kernel flow in fuel-fed prechambers |
US9653886B2 (en) | 2015-03-20 | 2017-05-16 | Woodward, Inc. | Cap shielded ignition system |
US9765682B2 (en) | 2013-06-10 | 2017-09-19 | Woodward, Inc. | Multi-chamber igniter |
US9797296B2 (en) | 2013-03-15 | 2017-10-24 | Cummins Inc. | Pre-chamber for internal combustion engine |
US9840963B2 (en) | 2015-03-20 | 2017-12-12 | Woodward, Inc. | Parallel prechamber ignition system |
US9890689B2 (en) | 2015-10-29 | 2018-02-13 | Woodward, Inc. | Gaseous fuel combustion |
US9893497B2 (en) | 2010-11-23 | 2018-02-13 | Woodward, Inc. | Controlled spark ignited flame kernel flow |
US10006358B2 (en) | 2011-07-28 | 2018-06-26 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10041402B2 (en) | 2016-05-12 | 2018-08-07 | Pratt & Whitney Canada Corp. | Internal combustion engine with split pilot injection |
US20180258834A1 (en) * | 2015-12-21 | 2018-09-13 | Mitsubishi Heavy Industries Engine & Turbocharger Ltd. | Precombustion-chamber engine |
US10125676B2 (en) | 2011-07-28 | 2018-11-13 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10145291B1 (en) | 2017-10-10 | 2018-12-04 | Pratt & Whitney Canada Corp. | Rotary engine and method of combusting fuel |
US10544732B2 (en) | 2011-07-28 | 2020-01-28 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with removable subchamber insert |
US10557407B2 (en) | 2011-07-28 | 2020-02-11 | Pratt & Whitney Canada Corp. | Rotary internal combustion engine with pilot subchamber |
US10557403B2 (en) | 2018-01-31 | 2020-02-11 | Fca Us Llc | Venturi-based purge vapor supply system for turbulent jet ignition engines |
US10801394B2 (en) | 2017-11-29 | 2020-10-13 | Pratt & Whitney Canada Corp. | Rotary engine with pilot subchambers |
US10883413B2 (en) | 2015-10-08 | 2021-01-05 | Cummins Inc. | Pre-chamber assembly |
US20220056836A1 (en) * | 2018-12-21 | 2022-02-24 | Innio Jenbacher Gmbh & Co Og | Cylinder head for an internal combustion engine |
US20220074341A1 (en) * | 2018-12-21 | 2022-03-10 | Innio Jenbacher Gmbh & Co Og | Cylinder head for an internal combustion engine |
US11359590B1 (en) * | 2021-05-26 | 2022-06-14 | Caterpillar Inc. | Igniter for dual fuel engine having liquid fuel outlet checks and spark ignition source |
US11408329B2 (en) * | 2019-12-19 | 2022-08-09 | Board Of Trustees Of Michigan State University | Engine turbulent jet ignition system |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110108009A1 (en) * | 2006-04-18 | 2011-05-12 | Megaion Research Corporation | System and method for preparing an optimized fuel mixture |
US8800536B2 (en) * | 2006-04-18 | 2014-08-12 | Megaion Research Corporation | System and method for preparing an optimized fuel mixture |
US8667951B2 (en) * | 2006-04-18 | 2014-03-11 | Megaion Research Corporation | System and method for preparing an optimized fuel mixture |
KR101359149B1 (en) * | 2009-11-13 | 2014-02-05 | 현대중공업 주식회사 | Pre-chamber for gas engine |
AT509876B1 (en) * | 2010-08-20 | 2011-12-15 | Ge Jenbacher Gmbh & Co Ohg | pre-chamber system |
KR101307080B1 (en) * | 2011-07-19 | 2013-09-11 | 현대중공업 주식회사 | Pre combustion chamber for gas engine |
JP6076662B2 (en) * | 2012-09-20 | 2017-02-08 | 三菱重工業株式会社 | Sub-chamber gas engine |
WO2015060236A1 (en) * | 2013-10-21 | 2015-04-30 | 三菱重工業株式会社 | Prechamber type gas engine |
JP6366262B2 (en) * | 2013-12-10 | 2018-08-01 | キヤノン株式会社 | Information processing apparatus, control method for information processing apparatus, and program |
JP2015117582A (en) * | 2013-12-16 | 2015-06-25 | 三菱重工業株式会社 | Gas engine and assembling method of gas engine |
WO2015136143A1 (en) * | 2014-03-13 | 2015-09-17 | Wärtsilä Finland Oy | Prechamber arrangement, cylinder head and piston engine |
EP2977582B1 (en) * | 2014-07-22 | 2018-03-28 | Caterpillar Energy Solutions GmbH | Ignition device with pre-combustion chamber |
WO2016028760A1 (en) | 2014-08-18 | 2016-02-25 | Woodward, Inc. | Torch igniter |
EP3012431B1 (en) * | 2014-10-21 | 2017-11-22 | Caterpillar Energy Solutions GmbH | Pre-combustion chamber assembly for internal combustion engines |
US9593622B2 (en) * | 2015-02-09 | 2017-03-14 | Caterpillar Inc. | Combustion system, nozzle for prechamber assembly, and method of making same |
US20170089252A1 (en) * | 2015-09-30 | 2017-03-30 | Caterpillar Inc. | Ignition plugs in prechamber and main combustion chamber of an ic engine |
US20160053668A1 (en) * | 2015-11-02 | 2016-02-25 | Caterpillar Inc. | Prechamber assembly for engine |
US10208651B2 (en) * | 2016-02-06 | 2019-02-19 | Prometheus Applied Technologies, Llc | Lean-burn pre-combustion chamber |
US10724423B2 (en) * | 2017-02-16 | 2020-07-28 | Caterpillar Inc. | Vented pre-chamber assembly for an engine |
US11421601B2 (en) | 2019-03-28 | 2022-08-23 | Woodward, Inc. | Second stage combustion for igniter |
EP4330525A1 (en) | 2021-04-28 | 2024-03-06 | Innio Jenbacher GmbH & Co OG | Pre-chamber assembly |
MX2024005639A (en) * | 2021-11-09 | 2024-07-29 | M2X Energy Inc | Pre-chamber combustion systems and methods. |
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2004
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-
2005
- 2005-09-27 WO PCT/NO2005/000357 patent/WO2006043818A1/en active Application Filing
- 2005-09-27 KR KR1020077009703A patent/KR100954004B1/en active IP Right Grant
- 2005-09-27 US US11/664,077 patent/US7950364B2/en active Active
- 2005-09-27 EP EP05795730.0A patent/EP2054593B1/en not_active Revoked
- 2005-09-27 ES ES05795730.0T patent/ES2501265T3/en active Active
- 2005-09-27 DK DK05795730.0T patent/DK2054593T3/en active
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Cited By (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120103302A1 (en) * | 2010-11-01 | 2012-05-03 | William Attard | Turbulent jet ignition pre-chamber combustion system for spark ignition engines |
US8857405B2 (en) * | 2010-11-01 | 2014-10-14 | Mahle Powertrain, Llc | Turbulent jet ignition pre-chamber combustion system for spark ignition engines |
US9353674B2 (en) | 2010-11-01 | 2016-05-31 | Mahle Powertrain, Llc | Turbulent jet ignition pre-chamber combustion system for spark ignition engines |
US9476347B2 (en) | 2010-11-23 | 2016-10-25 | Woodward, Inc. | Controlled spark ignited flame kernel flow in fuel-fed prechambers |
US11674494B2 (en) | 2010-11-23 | 2023-06-13 | Woodward, Inc. | Pre-chamber spark plug with tubular electrode and method of manufacturing same |
US10907532B2 (en) | 2010-11-23 | 2021-02-02 | Woodward. Inc. | Controlled spark ignited flame kernel flow in fuel-fed prechambers |
US9172217B2 (en) | 2010-11-23 | 2015-10-27 | Woodward, Inc. | Pre-chamber spark plug with tubular electrode and method of manufacturing same |
US9893497B2 (en) | 2010-11-23 | 2018-02-13 | Woodward, Inc. | Controlled spark ignited flame kernel flow |
US20120325179A1 (en) * | 2011-06-22 | 2012-12-27 | Caterpillar Inc. | Pre-combustion chamber tip |
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Also Published As
Publication number | Publication date |
---|---|
EP2054593B1 (en) | 2014-06-11 |
KR100954004B1 (en) | 2010-04-20 |
DK2054593T3 (en) | 2014-09-15 |
NO20044078L (en) | 2006-03-28 |
NO20044078D0 (en) | 2004-09-27 |
US20100132660A1 (en) | 2010-06-03 |
EP2054593A4 (en) | 2011-10-05 |
EP2054593A1 (en) | 2009-05-06 |
WO2006043818A1 (en) | 2006-04-27 |
NO322345B1 (en) | 2006-09-18 |
ES2501265T3 (en) | 2014-10-01 |
KR20070097025A (en) | 2007-10-02 |
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